EGYPTSAT A, 44047
Orbit data source: Space-Track
EGYPTSAT A, 44047 is a payload satellite owned by EgSA (EG) in SSO that was launched on Thu, 21 Feb 2019 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44047 intel report (Beta)
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Identifier
Orbit
Country
EG / EGYPRelated business
Manufacturer
Yuzhnoe
Mission
Operational Civil Imaging
Bus & Motor
EGYPTSAT, Unknown motor
Mass
~1,050 kg wet, ~1,050 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan + 1 Ant, 1.0 m
Radar Cross Section
0.867 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 EGYPTSAT A
1 44047U 19008A 26172.49277352 .00000909 00000-0 15161-3 0 9999
2 44047 98.0187 237.1963 0001386 99.1383 260.9981 14.72313459393870Epoch: 2026-06-21T11:49Z
TLE epoch observation values (Epoch: 2026-06-21T11:49:35.632Z)
Latitude
-0.00002°
Longitude
150.10558°
Altitude
656.852 km
Speed
7.529 km/s
True Right ascension
15h 48m 47s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:39:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.723 km
Perigee altitude
649.775 km
Semi-major axis
7,028.886 km
Eccentricity
0.00014
Inclination
98.0187°
RAAN
237.1963°
Arg. of periapsis
99.1383°
True anomaly
260.98241°
Mean anomaly
260.9981°
Eccentric anomaly
260.99026°
Mean motion
3.6831 °/min
Orbital period
97.74 mins
BSTAR
0.00015161
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Other satellites on launch #8 in the year 2019 (2019-02-21 UTC)
No other RSOs were in this launch
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EGYPTSAT A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 16:09:27.148Z | 59.014° ENE | 2026-06-22 16:11:27.148Z | 88.976° E | 16.768° | 2026-06-22 16:14:27.148Z | 133.008° SE |
| 7 mins | 2026-06-22 17:45:27.148Z | 351.985° N | 2026-06-22 17:48:27.148Z | 294.423° NW | 33.123° | 2026-06-22 17:52:27.148Z | 220.619° SW |
| 6 mins | 2026-06-23 04:44:27.148Z | 195.828° SSW | 2026-06-23 04:46:27.148Z | 239.78° WSW | 36.31° | 2026-06-23 04:50:27.148Z | 332.59° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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